20000808025879I

Incident

FAA incident report · Piper PA-28RT-201 · Eugene, OR · August 8, 2000

Date
August 8, 2000 · 12:15 local
Place
Eugene, OR
Phase of flight
Practice Training Manuevers
Operating rules
General operating rules (Part 91)
Aircraft
N8108M
Reported as
Piper PA28RT201
Reported engine
Continental IO360*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
337 total160 in this make and model110 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) During an instructional flight, the instructor noticed a loss of power in manuevering flight with the power initially set at 21' mp at 2200 RPM. An increase in oil temperature was noted although the oil pressure remained constant and within normal ranges. The a/c was turned back to the Eugene, Oregon airport when a severe vibration was experienced and the engine was shut down to prevent structural damage. An emergency landing was performed to the ground in a nearby hay field. There was no damage to the a/c, and no injuries occurred. FAA maintenance personnel inspected the engine and found bearing material throughout the oil system. Further investigation revealed rear main bearing failure leading to crankshaft fatigue separation at the number 4 crankshaft pin.

As the FAA filed it

(-23) DURING AN INSTRUCTIONAL FLIGHT, THE INSTRUCTOR NOTICED A LOSS OF POWER IN MANUEVERING FLIGHT WITH THE POWER INITIALLY SET AT 21' MP AT 2200 RPM. AN INCREASE IN OIL TEMPERATURE WAS NOTED ALTHOUGH THE OIL PRESSURE REMAINED CONSTANT AND WITHIN NORMAL RANGES. THE A/C WAS TURNED BACK TO THE EUGENE, OREGON AIRPORT WHEN A SEVERE VIBRATION WAS EXPERIENCED AND THE ENGINE WAS SHUT DOWN TO PREVENT STRUCTURAL DAMAGE. AN EMERGENCY LANDING WAS PERFORMED TO THE GROUND IN A NEARBY HAY FIELD. THERE WAS NO DAMAGE TO THE A/C, AND NO INJURIES OCCURRED. FAA MAINTENANCE PERSONNEL INSPECTED THE ENGINE AND FOUND BEARING MATERIAL THROUGHOUT THE OIL SYSTEM. FURTHER INVESTIGATION REVEALED REAR MAIN BEARING FAILURE LEADING TO CRANKSHAFT FATIGUE SEPARATION AT THE NUMBER 4 CRANKSHAFT PIN.